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SYSTEM DESCRIPTION AND INSTALLATION MANUAL

HS--600 High Speed Data System

23--20--31

30 May 2002

Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.

Page 7--3

(2) Reinstall the combiner.

(a) Attach the combiner using six screws.

(b) Remove the protective covers from the connectors and install the aircraft

connectors on the combiner.

(3) Remove the splitter.

(a) Remove power from the HSU. Circuit breakers for the HSU are typically located

on the flight deck.

(b) Locate the splitter.

on the connectors.

(d) Remove the two screws holding the splitter in position.

(4) Reinstall the splitter.

(a) Attach the splitter using two screws.

(b) Remove the protective covers from the connectors and install the aircraft

connectors on the splitter.

B. Adjustment Procedures

(1) Not applicable.

C. Repair Procedures

(1) Not applicable.

D. Return to Service Procedures

(1) Refer to test procedures in the INSTALLATION CHECK section of this manual.

Summary of Contents for HS-600

Page 1: ...States in accordance with the export administration regulations Diversion contrary to U S law is prohibited Honeywell Aerospace Electronic Systems CES Phoenix P O Box 21111 Phoenix Arizona 85036 1111 U S A Printed in U S A Pub No A15 5111 006 23 20 31 Title Page T 1 30 May 2002 System Description and Installation Manual HS 600 High Speed Data System ...

Page 2: ...xtent required for installation or maintenance of the recipient s equipment NOTICE FREEDOM OF INFORMATION ACT 5 USC 552 AND DISCLOSURE OF CONFIDENTIAL INFORMATION GENERALLY 18 USC 1905 This document is being furnished in confidence by Honeywell The information disclosed herein fall within exemption b 4 of 5 USC 552 and the prohibitions of 18 USC 1905 S2002 Honeywell is a U S registered trademark o...

Page 3: ... is based on electronic form INF 300 Revision 0 To help us improve the quality of our publication Honeywell encourages any report of a possible data error PUBLICATION INFORMATION Publication Number A15 5111 006 Volume No Book or Addendum ATA Number 23 20 31 Latest Issue Date From Title Page Publication Title High Speed Data Unit Document Type System Description and Installation Manual READER INFOR...

Page 4: ...IT NO 3532 PHOENIX AZ FOLD FOLD POSTAGE WILL BE PAID BY ADDRESSEE Honeywell Aerospace Electronic Systems CES Phoenix P O Box 21111 Phoenix Arizona 85036 1111 U S A ATTN Technical Publications Quality Administrator NO POSTAGE NECESSARY IF MAILED IN THE UNITED STATES ...

Page 5: ...t Issue Date From Title Page Publication Title High Speed Data Unit Document Type System Description and Installation Manual READER INFORMATION Please check all that apply h Trainer h Technician h Librarian h Engineer h Other Please specify Your Name optional Company Name Street Address City State Province Street Address City State Province Zip Code Country Telephone No FAX No CUSTOMER SATISFACTIO...

Page 6: ...IT NO 3532 PHOENIX AZ FOLD FOLD POSTAGE WILL BE PAID BY ADDRESSEE Honeywell Aerospace Electronic Systems CES Phoenix P O Box 21111 Phoenix Arizona 85036 1111 U S A ATTN Technical Publications Quality Administrator NO POSTAGE NECESSARY IF MAILED IN THE UNITED STATES ...

Page 7: ...nt Page RR 1 RECORD OF REVISIONS For each revision put the revised pages in your manual and discard the superseded pages Write the revision number and date date put in manual and the incorporator s initials in the applicable columns on the Record of Revisions The initial H shows Honeywell is the incorporator Revision Number Revision Date Date Put In Manual By Revision Number Revision Date Date Put...

Page 8: ...ON AND INSTALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page RR 2 Blank Page ...

Page 9: ...IONS Instructions on each page of a temporary revision tell you where to put the pages in your manual Remove temporary revision pages only when discard instructions are given For each temporary revision put the applicable data in the record columns on this page Temporary Revision Number Temporary Revision Date Temporary Revision Status Date Put in Manual By Date Removed from Manual By The initial ...

Page 10: ...N AND INSTALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page RTR 2 Blank Page ...

Page 11: ...d Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page SBL 1 SERVICE BULLETIN LIST Service Bulletin Identified Mod Date Included in this Manual Description ...

Page 12: ...N AND INSTALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page SBL 2 Blank Page ...

Page 13: ...y 2002 TC 5 30 May 2002 TC 6 30 May 2002 Introduction INTRO 1 30 May 2002 INTRO 2 30 May 2002 INTRO 3 30 May 2002 INTRO 4 30 May 2002 System Description and Operation 1 1 30 May 2002 1 2 30 May 2002 1 3 30 May 2002 1 4 30 May 2002 1 5 30 May 2002 1 6 30 May 2002 1 7 30 May 2002 1 8 30 May 2002 1 9 30 May 2002 1 10 30 May 2002 1 11 30 May 2002 1 12 30 May 2002 1 13 30 May 2002 1 14 30 May 2002 Mech...

Page 14: ...02 5 5 30 May 2002 5 6 30 May 2002 5 7 30 May 2002 5 8 30 May 2002 Fault Isolation 6 1 30 May 2002 6 2 30 May 2002 Maintenance Practices 7 1 30 May 2002 7 2 30 May 2002 7 3 30 May 2002 7 4 30 May 2002 M4 Call Cause Code List A 1 30 May 2002 A 2 30 May 2002 A 3 30 May 2002 A 4 30 May 2002 A 5 30 May 2002 A 6 30 May 2002 A 7 30 May 2002 A 8 30 May 2002 A 9 30 May 2002 A 10 30 May 2002 Inmarsat Regis...

Page 15: ...CONTENTS ...

Page 16: ...his Manual INTRO 2 B Weights and Measurements INTRO 3 C Acronyms and Abbreviations INTRO 3 3 Customer Assistance INTRO 4 A Who to Contact INTRO 4 SYSTEM DESCRIPTION AND OPERATION 1 1 1 Overview 1 1 A General 1 1 B Aero H H 1 3 C Inmarsat High Speed Systems 1 3 D System Performance 1 4 E FCC Compliance 1 5 2 System Components 1 6 A General 1 6 3 Component Descriptions 1 7 A HS 600 High Speed Data U...

Page 17: ...s 3 1 2 Electrical Installation Procedure 3 1 A General 3 1 B Power Requirements 3 1 C Ground Requirements 3 2 1 General 3 2 2 Chassis Grounding 3 2 3 Shield Grounds 3 3 4 Power Signal Grounds 3 4 3 Electrical Installation 3 5 A HS 600 HSU 3 5 INSTALLATION CHECK 4 1 1 Overview 4 1 A General 4 1 2 Installation Checkout 4 1 A General 4 1 B Cable Loss Checks 4 1 1 HS 600 HSU to HPA Path Loss 4 1 2 HP...

Page 18: ...ment and Materials 7 1 2 Procedure for the HS 600 HSU 7 1 A Removal and Reinstallation Procedures 7 1 B Adjustment Procedures 7 2 C Repair Procedures 7 2 D Return to Service Procedures 7 2 3 Procedure for the Combiner Splitter 7 2 A Removal and Reinstallation Procedures 7 2 B Adjustment Procedures 7 3 C Repair Procedures 7 3 D Return to Service Procedures 7 3 4 Instructions for Continued Airworthi...

Page 19: ...2 9 Figure 2 4 Typical Dimensions for 4 MCU Tray Assemblies 2 10 Figure 2 5 Typical Dimensions for 8 MCU Tray Assemblies 2 11 Figure 3 1 Electric Cable Chart 3 2 Figure 3 2 Example 1 Multi point Shield Ground 3 3 Figure 3 3 Example 2 Multi point Shield Ground 3 3 Figure 3 4 Shield Grounding Example for Rack Mount Connectors 3 4 Figure 3 5 Aircraft Grounding 3 5 Figure 3 6 HSU ARINC 600 Connector P...

Page 20: ...ith Aero H Global beam operation and 10 5 Kbps Packet Data Rate 1 5 Table 1 9 Total Number of Calls with Aero H Global beam operation and 600 bps Packet Data Rate 1 5 Table 1 10 Components Supplied by Honeywell 1 6 Table 1 11 Components Parts Not Supplied by Honeywell 1 6 Table 1 12 HS 600 Leading Particulars 1 9 Table 1 13 DO 160D Environmental Categories 1 10 Table 1 14 HSU Front Panel Light Des...

Page 21: ...ON AND INSTALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page TC 6 Blank Page ...

Page 22: ...INTRODUCTION ...

Page 23: ...002 Honeywell All Rights Reserved 3 Honeywell is a U S registered trademark of Honeywell All other marks are owned by their respective companies B Export Notice 1 This document contains unrestricted technical data and is being exported under license exception TSU OTS in accordance with EAR Section 740 13 a 2 These commodities technology or software were exported from the United States in accordanc...

Page 24: ...is Manual 1 This manual gives general system description and installation information for the HS 600 High Speed Data System It also gives block diagram and interconnect information to permit a general understanding of the system interface 2 The purpose of this manual is to help you install operate maintain and troubleshoot the HS 600 High Speed Data System Common system maintenance procedures are ...

Page 25: ...260 Term Definition ACSE access control and signalling equipment ACU antenna control unit BSU beam steering unit CCA circuit card assembly CMT commissioning and maintenance terminal CNS ATM communication navigation and surveillance air traffic management DLNA diplexer low noise amplifier DLT data logging terminal ESD electrostatic discharge ESDS electrostatic discharge sensitive HGA high gain ante...

Page 26: ...tion number PSTN Public Switched Telephone Network RF radio frequency RFU radio frequency unit SATCOM satellite communications SCPC single channel per circuit SDM System Definition Manual SDU satellite data unit SU signal unit TDM time division multiplex TDMA time division multiple access 3 Customer Assistance A Who to Contact 1 For assistance with installation operation or maintenance of the HS 6...

Page 27: ...SYSTEMS DESCRIPTION AND OPERATION ...

Page 28: ...y notice of this document Page 1 1 SECTION 1 SYSTEM DESCRIPTION AND OPERATION 1 Overview A General 1 The HS 600 high speed data system provides multi channel Inmarsat Aero cockpit and passenger voice fax and data and multi media mini M M4 circuit mode services simultaneously Figure 1 1 shows a block diagram of the high speed data HSD system Figure 1 1 High Speed Data System Block Diagram ...

Page 29: ...cations and operates without knowledge of the HSD system presence However each SDU used in conjunction with the HSD system will require advance configuration of its data logging terminal DLT parameter settings 5 The SDU s DLT RS 232 port must be configured to transmit the ASCII data given in Table 1 1 at a rate of approximately 1 Hz for the functions in Table 1 1 to be performed in the HSD system ...

Page 30: ...as given in Table 1 3 Table 1 3 Type of Service Aero Type Antenna Global Beam Spot Beam Voice 9 6 kbps Voice 4 8 kbps Secure Voice 4 8 kbps Fax max PC Data max Packet Mode Data max Aero H High gain Yes No Yes No Yes 4 8 kbps 2 4 kbps 10 5 kbps Aero H High gain Yes Yes Yes Yes Yes 4 8 2 4 kbps 2 4 kbps 10 5 kbps 2 When used within the spot beams Aero H voice and data rates are lower Therefore it re...

Page 31: ...Item dB Watts Gain cell 12 dB R T power 10 5 Kbps assumed 20 4 dBW 109 6 W R T power 600 bps assumed 5 9 dBW 3 9 W HPA power same assumed for both 16 0 dBW 40 0 W Cable Loss 4 7 dB Initial HSD channel power 22 5 dBW 177 8 W Settled HSD channel power 22 5 dBW 177 8 W Initial 8400 C channel EIRP 14 5 dBW 28 2 W Settled 8400 C channel EIRP 7 5 dBW 5 6 W Initial 21000 C channel EIRP 19 5 dBW 89 1 W Se...

Page 32: ...hannels 1 0 1 2 Table 1 9 Total Number of Calls with Aero H Global beam operation and 600 bps Packet Data Rate M4 HSD Channels 8400 Voice Channels 21000 Voice Channels 1 0 5 2 From these calculations the following points should be made a There is an increased loss of 3 5 dB due to the addition of the high power combiner with the HS 600 installation It is essential that a 12 dB antenna is used to b...

Page 33: ...l Part No High Speed Data Unit HS 600 7519300 901 High Speed Combiner Assembly 7519340 901 RF Power Splitter 7519349 1 High Power Amplifier 40 W HP 600 7516250 XX050 Note NOTE The HSD system requires an additional HPA Only an HPA Part No 7516250 XX050 software Mod F can be used with the HS 600 system Table 1 11 Components Parts Not Supplied by Honeywell Component Part Comments HSU Mounting Tray 4 ...

Page 34: ...t card assembly CCA All CCAs are built to standards that qualify them for both airline and business aircraft usage 2 The HSU is packaged as a 4 modular concept unit 4 MCU The mechanical chassis is constructed of aluminum alloy sheet metal The HSU requires external cooling air in accordance with ARINC 600 or ARINC 404 to maintain the highest possible mean time between failures MTBF In installations...

Page 35: ...D INSTALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 1 8 Figure 1 2 HS 600 HSU ...

Page 36: ...ments DC Note Nominal 27 5 V dc Maximum 32 2 V dc Minimum 20 5 V dc Power Consumption 25 W nominal 40 W maximum Cooling Requirements Select tray from Table 1 15 Connector P1 Rear Radiall Part No 620 600 237 Mating Connector P1 Radiall Part No 620 600 238 22 AWG Contacts Radiall Part No 620 200 20 AWG Contacts Radiall Part No 620 310 16 AWG Contacts Radiall Part No 620 330 12 AWG Contacts Radiall P...

Page 37: ...perature and Altitude XX In Flight Loss of Cooling X Temperature Variation X Humidity X Shock B Vibration SB2 Explosion Proofness X Waterproofness X Fluids Susceptibility X Sand and Dust X Fungus Resistance X Salt Spray X Magnetic Effect X Power Input X Voltage Spike X Audio Frequency Susceptibility X Induced Signal Susceptibility X Radio Frequency RF Susceptibility XXX Emission of RF Energy M Lig...

Page 38: ...ithin 30 seconds of power up Receiver Activity If the SDU is logged on the HS 600 is able to pick an LES to listen to similar to the P channel for the MCS Once the receiver synchronizes on this time division multiplex TDM channel the green PASS light flashes The light flashes for each correctly received signal unit SU This should occur within 2 minutes of power up if the SDU is logged on or within...

Page 39: ...ion on this page is subject to the restrictions in the proprietary notice of this document Page 1 12 B High Speed Combiner Assembly 1 The high speed combiner assembly combines the signals from both HPAs which are then sent to the DLNA Figure 1 3 shows the high speed combiner assembly Figure 1 3 High Speed Combiner Assembly ...

Page 40: ...then sent to the SDU and HSU The unit weight is 2 5 oz 70 87 grams Figure 1 4 shows the RF power splitter Figure 1 4 RF Power Splitter D HSU Mounting Tray 1 The HS 600 HSU ARINC 600 connector contacts and mounting trays can be purchased from ECS or EMTEQ The addresses for ECS and EMTEQ are as follows Electronic Cable Specialists 5300 W Franklin Drive Franklin WI 53132 U S A Telephone 414 421 5300 ...

Page 41: ...MCU S S tray with bottom fan 115 V ac 6049 101 4 MCU S S tray with right side fan 115 V ac 6049 102 4 MCU S S tray with left side fan 115 V ac 6083 102 4 MCU S L tray with rear fan 115 V ac 6050 102 4 MCU S S tray with bottom fan 28 V dc 200 89891 101 4 MCU S S tray with left side fan 28 V dc 200 89892 101 4 MCU S S tray with right side fan 28 V dc 6083 103 4 MCU S L tray with rear fan 28 V dc 629...

Page 42: ...MECHANICAL INSTALLATION ...

Page 43: ...nstallation Design A HS 600 HSU Provisions 1 Mechanical installation data for the HS 600 HSU is shown in Figure 2 1 The HSU is mounted in an ARINC 600 4 MCU mounting tray The HSU requires external cooling air to maintain the highest possible MTBF A mounting tray with an integral fan is required Select a mounting tray from Table 1 15 Figure 2 4 shows typical 4 MCU tray assemblies with a fan 2 The l...

Page 44: ...ON AND INSTALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 2 2 Blank Page ...

Page 45: ...AL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 2 3 2 4 Figure 2 1 Sheet 1 HSU Outline and Installation Diagram ...

Page 46: ...AL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 2 5 2 6 Figure 2 1 Sheet 2 HSU Outline and Installation Diagram ...

Page 47: ...S 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 2 7 2 8 Figure 2 2 High Speed Combiner Outline and Installation Diagram ...

Page 48: ...ON MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 2 9 Figure 2 3 RF Power Splitter Outline Diagram ...

Page 49: ...UAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 2 10 Figure 2 4 Typical Dimensions for 4 MCU Tray Assemblies ...

Page 50: ...UAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 2 11 Figure 2 5 Typical Dimensions for 8 MCU Tray Assemblies ...

Page 51: ...ON AND INSTALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 2 12 Blank Page ...

Page 52: ...ELECTRICAL INSTALLATION ...

Page 53: ... 5 Under all load conditions amplitude modulation of the power supply will not exceed 2 at any frequency Percent modulation is defined as one half of the peak to peak modulation envelope divided by the carrier amplitude and multiplied by 100 2 DC Power The aircraft dc power supply must be 28 V dc nominal The normal minimum and maximum voltages permitted are 20 5 and 32 2 V dc respectively 3 Power ...

Page 54: ...omagnetic frequencies HIRF and lightning environments You must obey this section to satisfy these requirements NOTE HIRF and lightning requirements dictate that the shielded wires meet the requirements of paragraph 2 C 3 Installation of this system into aircraft manufactured prior to the FAA requirements adheres to these practices whenever feasible 2 Chassis Grounding a All rack mount remote mount...

Page 55: ...ween the LRU mounting tray or LRU itself if a tray is not used and the nearest airframe grounding point 3 Shield Grounds a The shield wires in the HSU have the shield grounded at both ends This is called multi point grounding and is specified to minimize the adverse effects of HIRF and lightning b The shield must not be connected to any LRU or bulkhead connector pin c Examples of multi point shiel...

Page 56: ...ed together all signal grounds are tied together and all lighting grounds are tied together DC power ac power signal and light ground groups are then tied together at a single point and connected to the airframe Figure 3 5 shows this aircraft grounding method NOTE It is very important this grounding technique be adhered to Do not tie the various ground wires to multiple aircraft frame points and d...

Page 57: ...various remote signal ground blocks must all be grounded only at the aircraft central grounding point If 10 signal grounds are connected to a remote terminal block a minimum of one grounding wire must be run from this terminal block to the aircraft central grounding point 3 Electrical Installation A HS 600 HSU 1 The HSU rear ARINC 600 connector layout is shown in Figure 3 6 The contact arrangement...

Page 58: ... MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 3 6 Figure 3 6 HSU ARINC 600 Connector P1 Pin Layout ...

Page 59: ...C RXD ISDNU RING ASYNC DSR SIG GND ASYNC RTS SIG GND RSVD SPARE 199 RSVD SPARE 212 RSVD SPARE 103 RSVD SPARE 115 CHASSIS GND RSVD VHF KEYLINE GND 8 RSVD SPARE LO 26 RSVD SPARE HI 26 RSVD SPARE LO 27 RSVD SPARE HI 27 RSVD SPARE HI 11 RSVD SPARE LO 11 RSVD SPARE 36 RSVD SPARE 85 RSVD SPARE HI 4 RSVD SPARE LO 4 9 RSVD VHF AUDIO OUT HI RSVD VHF AUDIO OUT LO RSVD VHF AUDIO IN HI RSVD VHF AUDIO IN LOW R...

Page 60: ...VD SPARE HI 18 RSVD SPARE LO 18 RSVD SPARE 41 RSVD SPARE 90 7 RSVD SPARE HI 19 RSVD SPARE LO 19 RSVD SPARE 32 RSVD SPARE 81 RSVD SPARE 253 RSVD SPARE HI 2 RSVD SPARE LO 2 CHASSIS GND RSVD SPARE 15 RSVD SPARE 64 8 RSVD SPARE 42 RSVD SPARE 91 RSVD SPARE 27 RSVD SPARE 76 RSVD SPARE 47 RSVD SPARE 96 RSVD SPARE 38 RSVD SPARE 87 RSVD SPARE 35 RSVD SPARE 84 9 RSVD SPARE HI 15 RSVD SPARE LO 15 RSVD SPARE ...

Page 61: ... 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 3 9 Figure 3 7 Contact Arrangements for P1 C Bottom Insert HSU ARINC 600 Connector Figure 3 8 HSU Data Loader Connector J1 Pin Layout ...

Page 62: ...TALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 3 10 Figure 3 9 RF System Interface ...

Page 63: ...L HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 3 11 3 12 Figure 3 10 High Speed Data System Interconnect Diagram ...

Page 64: ...INSTALLATION CHECK ...

Page 65: ...d connector losses between the HSU TX output BP13 to the HPA RF input TP1C b If necessary install an attenuator to achieve a total loss of 19 21 dB 2 HPA to Antenna Loss a Measure the total loss between the HS 600 HPA RF output MP1C to the antenna RF port J2 b Enter this value into parameter No 5 through the HS 600 maintenance port Do no change any other parameters Do no forget to save the changes...

Page 66: ...1 005 for installation details D RF Checks 1 Check the pins listed in Table 4 2 Figure 4 1 shows the receive RX path loss and Figure 4 2 shows the transmit TX path loss These losses are achieved by a combination of RF coaxial cable losses and installed RF attenuators the latter if required Table 4 2 RF Checks From LRU Connector Pin To LRU Connector Pin RX Splitter RX IN DLNA J2 RX OUT RX OUT MCS 3...

Page 67: ...N MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 4 3 Figure 4 1 RX Path Loss Figure 4 2 TX Path Loss ...

Page 68: ...ON AND INSTALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 4 4 Blank Page ...

Page 69: ...ADJUSTMENT TEST ...

Page 70: ...perate with a PC the initial settings of the maintenance port must be as follows Speed normally 115 200 bps 8 data bits No parity 1 stop bit Turn caps lock ON B Software 1 The software can be any communications package that can send and receive ASCII at 115 200 baud rate 8 bits with no parity bit and 1 stop bit Among the programs that have been used are ProComm and HyperTerminal from Windows C Sys...

Page 71: ... the periodic data word setup 6 Align the inertial reference system IRS 7 Remove the cable from the SDU to the PC 8 Connect a cable from the HSU to the RS 232 maintenance port as given in Table 5 2 Table 5 2 HSU to RS 232 Maintenance Port Wire List From HSU Connector Pin To RS 232 Maintenance Port 9 Pin Female D Type Connector Pin TP6G 3 TP6F 2 TP6J TP6H 5 9 Connect a cable from the RS 232 mainten...

Page 72: ...ance Port Start Up Information 1 The information given in Table 5 3 is the typical output from the HS 600 maintenance port following a power cycle The information assumes that the IRS has aligned and the multi channel SATCOM has logged on Table 5 3 Typical HS 600 Maintenance Port Information M4 IDU BOOT HEADER 1 Download IDU Flash 2 Boot from Flash default wait Please input your choice Time Out Bo...

Page 73: ...lash memory ok issue no is 23 Waiting for LOG ON message from HTCE Power Control PH 0 15 0 EIRP 0 25 0 PM 0 9 5 GH 0 58 0 Obo 0 2 0 Set Economy Flag 0 IIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIII Press ENTER to start Maintenance Setting EIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIII 00 900 APP SM SM_CONFIG_CO ff ff f...

Page 74: ...lletin Board Update Ok Issue No 23 CHNL 0 T 14300 STATE CHANGE FROM 2 3 CHNL 0 T 14300 BB Update Ok wait for SBS finishing CHNL 0 T 14300 Init ReInit SBS CHNL 0 T 14300 SBS started Position Lat 33 000000 Long 112 003326 CHNL 0 SBS ID 6 CHNL 0 T 14303 SBS finished CHNL 0 Rx is 24cc CHNL 0 T 14304 STATE CHANGE FROM 3 6 CHNL 0 T 14304 Start ocean region registration CHNL 0 T 14306 get sync on NCRA ch...

Page 75: ... 2 Ref oscillator correction factor 125Hz 3 Transmit Doppler compensation adjustment rate 60Hz sec 4 G M H ISE MTU to HPA output gain 40dB 5 HPA output to antenna input loss 2dB 6 G Amin Minimum usable reported antenna gain 7dB 7 P omin Max allowed HPA average output power 17 0dBW 8 Enabled BEARE Service Interface 0 9 Min Frame No for TX port 3 A HPA Format Selection N S Save setting and Exit EIII...

Page 76: ...on 6 Minimum usable reported antenna gain below which the ISE ceases operation of the HSD channel range 7 to 12 dB in 1dB steps 7Hz Please enter new value between 7 to 12 Keep current value Enter your selection 7 Maximum allowed HPA average output power range 20 to 60W or 13 to 18 dBW in 0 5dB steps 17 0Hz Please enter new value between 13 0 to 18 0 Keep current value Enter your selection 8 Enable...

Page 77: ...TE Must power cycle HS 600 for parameter save to take effect Main Menu 1 Protocol Mode 2 Manual Mode 3 Change Password Enter your selection 1 NOTE Press ESC ESC or power cycle to exit from this menu Menu in protocol mode 1 Event Log ESC Exit Enter your selection Menu in protocol mode 1 Event Log ESC Exit Enter your selection 1 Event Log Menu 1 Display last 20 Event Log records 2 Display specified ...

Page 78: ...FAULT ISOLATION ...

Page 79: ... HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 6 1 SECTION 6 FAULT ISOLATION 1 Overview A General 1 To be supplied ...

Page 80: ...ON AND INSTALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page 6 2 Blank Page ...

Page 81: ...MAINTENANCE PRACTICES ...

Page 82: ...d Materials 1 No additional special equipment or materials other than those commonly used in the shop are required to install the units in existing trays and clamps and adjust the system Do not over tighten mounting screws Where torque values are not given it is acceptable to finger tighten the mounting screws 2 Procedure for the HS 600 HSU A Removal and Reinstallation Procedures 1 Remove the HSU ...

Page 83: ...until its connectors are fully engaged with the mating connectors of the mounting tray e Put the holddown clamps in place and tighten the knobs in a clockwise direction until the proper torque is applied clutch engages f Reapply power to the HSU and its interfacing equipment NOTE Upon applying primary power the HSU will automatically power up and start a POST B Adjustment Procedures 1 Not applicab...

Page 84: ... power from the HSU Circuit breakers for the HSU are typically located on the flight deck b Locate the splitter c Disconnect the aircraft connectors from the splitter and place protective covers on the connectors d Remove the two screws holding the splitter in position 4 Reinstall the splitter a Attach the splitter using two screws b Remove the protective covers from the connectors and install the...

Page 85: ...craft Wiring Diagram Manuals 4 The high speed data system components are considered on condition units and no additional maintenance is required other than a check for security and operation at normal inspection intervals 5 If a system component is inoperative remove unit secure cables and wiring collar applicable switches and circuit breakers and placard them inoperative Revise equipment list and...

Page 86: ...APPENDIX A ...

Page 87: ... Failed to synchronize to the NCSA LESA channel frequency 0105 User cleared call before the single channel per circuit SCPC channel was assigned 0106 Failed to receive the channel assignment 0107 85H code instead of channel assignment received 0108 DSP failed to reset after call clear 0109 DSP failed to reset before loading the Mini M high speed data MM HSD service code 0110 DSP failed to load the...

Page 88: ...se subsequent to the acceptance of the call and the signaling of the identity of the mobile terminal to which the call will actually be routed that terminal has become out of service and therefore cannot be rung 1 1141 Call Cleared pre empted at MES MES clear pre emption for higher priority call 1 1142 Call Refused due to Distress Call from MES MES clear Fixed MES has initiated a distress call 1 1...

Page 89: ...is not consistent with the personal identification number PID information in the fixed MES originated PID and PID MES Registration Tables at the LES as it relates to this call 1 11D7 LES is failing the call because the service requested by the MES in the distress urgency or safety access request is not 4 8 kbps AMBE telephony 1 11D8 LES is clearing the call because the service address received fro...

Page 90: ...use a SCPC channel release SU type 8AH has not been received by the MES in response to the transmission of a notification acknowledge message type BAH during the supplementary services call diversion information retrieval process within the allowed time limit 1 12C8 Spot Beam Handover MES is clearing the call session in the next beam because the MES did not detect the LESH carrier on the new frequ...

Page 91: ...earing the call session in the current beam normal clear 1 1541 Call Cleared pre empted at LES LES clear pre empted by higher priority call 1 1551 Call Failed LES Congested No Channel LES is rejecting the call because an appropriate satellite channel is not currently available at this specific LES 1 1552 LES reject appropriate time division multiplex TDM time division multiple access TDMA time slo...

Page 92: ... by the LES within the allowed time limit 1 15C2 LES is clearing the call because the Service Address information has not been received by the LES from MES within the allowed time limit 1 15C3 Call Failed LES Timeout No Scrambling Vector LES is clearing the call because a Scrambling Vector message type 8D has not been received by the LES from the MES within the allowed time limit 1 15C4 Call Faile...

Page 93: ...in reception of the MES carrier exceeding the allowed time limit of 62 seconds 1 16C1 LES clear SEST carrier not received 1 16C2 LES is clearing the call because an appropriate SCPC MES carrier has not been received by the LES at the commencement of the call within the allowed time limit 1 16C3 Spot Beam Handover LES is clearing the call session in the next beam because the LES did not detect the ...

Page 94: ...pt for Distress calls at the NCS 1 18A3 NCS is rejecting the call because the specified LES is not authorized for the requested service at the NCS 1 18A4 Reserved 1 18B1 NCS is rejecting or clearing the call for a reason which is not covered by any of the currently defined Cause events 1 18B2 NCS is rejecting the call because the requested service variant is invalid 1 18C1 NCS is rejecting the cal...

Page 95: ...could be a problem with a particular LES channel unit The channel unit may need to be reset This cause code may also occur after the call has been connected This problem may also occur during an NCS outage 4 Check which ISP or AA commissioned the phone or smart card 5 Verify that the customer s smart card information including the Ki is entered in the ACE database at the LES For fixed 16 mobile ca...

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Page 97: ...APPENDIX B ...

Page 98: ... Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page B 1 APPENDIX B INMARSAT REGISTRATION FORM 1 Overview A General 1 This appendix provides an example of the Inmarsat registration form required to activate the HSD system ...

Page 99: ...CRIPTION AND INSTALLATION MANUAL HS 600 High Speed Data System 23 20 31 30 May 2002 Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document Page B 2 ...

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Honeywell HS-600, Description And Installation Manual

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